Timberwind 45 Propellants: Nuclear/LH2. Thrust(vac): 441.300 kN (99,208 lbf). Thrust(sl): 392.800 kN (88,305 lbf). Isp: 1,000 sec. Isp (sea level): 890 sec. Burn time: 449 sec. Mass Engine: 1,500 kg (3,300 lb). Diameter: 4.25 m (13.94 ft). Chambers: 1. Thrust to Weight Ratio: 30.00. Country: USA. Status: Development ended 1992. Timberwind 45 used on Rocket Stages Used on stage: Timberwind 45. on launch vehicle: Timberwind Centaur.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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